AIRPORT PLANNING MANUAL 2. AIRCRAFT DESCRIPTION 2.1. AIRCRAFT CHARACTERISTICS The aircraft is: • Predominantly metallic; • Low winged; • Conventional tailed; • Monoplane; • Retractable tricycle-type with twin-wheeled landing-gear. There are two high bypass ratio turbofan GEAE CF34–8E with 63.2 kN (14200 lbf) maximum takeoff thrust (sea level, static and ISA + 15 °C) installed under the wings. Theaircraft has two versions, with different ranges as a function of the difference between the MTOWs: • The STD aircraft model - MTOW 35990 kg (79344 lb) • The LR, SU or SE aircraft models - MTOW 37200 kg (82012 lb) 2.1.1. Definitions MRW It is the maximum allowed aircraft weight for taxiing or maneuvering on the ground. MLW It is the maximum allowed weight with which the aircraft can normally be landed. MTOW It is the maximum allowed total loaded aircraft weight at the start of the takeoff run. BOW It is the weight of the structure, powerplant, instruments, flight controls, hydraulic, electronic, electrical, air conditioning, oxygen, anti-icing and pressurization systems, interior furnishings, portable and emer- gency equipment and other items of equipment that are an integral part of the aircraft configuration. It also includes unusable fuel, total engine and APU oil, total hydraulic fluid, toilet fluid and water, potable water, crew and crew baggage, navigation kit (manuals, charts), catering (beverages and food) and removable service equipment for the galley. MZFW It is the maximum allowed weight without usable fuel in the tanks. EFFECTIVITY: ALL Section 2 Page 2-1 Oct 07/08 w-apm1346